Composites with one or multiple principal strengthening compounds and at least one principal cemented refractory metal

ABSTRACT

A composite composed of one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal that is prepared by combining a suitable binary to senary borides and/or carbides with a unitary to binary principal refractory metal is disclosed. As compared with the conventional sintered cemented carbides, the composite of the disclosure not only possess high hardness and high toughness but also has various ratios of principal components since it is not prepared with equal mole during the process.

CROSS-REFERENCE TO RELATED APPLICATION

This application also claims priority to Taiwan Patent Application No. 105102965 filed in the Taiwan Patent Office on Jan. 29, 2016, the entire content of which is incorporated herein by reference.

BACKGROUND OF THE INVENTION

1. Field of the Invention

The disclosure is related to a composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal, and is specifically related to suitable binary to senary borides and/or carbides combining with the principal cemented refractory metal and few other elements so as to prepare a composite with superior hardness and toughness.

2. Descriptions of the Related Art

Conventional cemented carbides are a group of composites composed of WC and Co. In the early 1900s, Henri Moissan synthesized tungsten carbide (WC). Tungsten carbide is of a high hardness, and therefore could be even replacing diamonds in certain applications. However, the tungsten carbide is so brittle and porous that it is not suitable in engineering applications. In 1923, Schröter and Baumhauer found that after being sintered with cobalt or nickel, the tungsten carbide can maintain the hardness of ceramics at no expense of the toughness of metals. Thus, it is beneficial in mould industry. The material has been widely used in different units of cutting tools, mineral extraction and military weapons. About 60% of W consumption is used in producing cemented carbides. In 1930, the demand was 10 tons, and in 2008, it was 50,000 tons, increased by 5000 times in 78 years.

Cemented carbides are with two parts, one is a hardening and strengthening phase, and the other a cementing or binding phase. As described above, when WC is in the strengthening phase it has a high melting point and a high toughness as well as being good in wear resistance. Co in the cemented phase could contribute to a high electrical and thermal conductivity as well as to a high toughness so that the composite is not brittle. In recent studies, hard metals, such as WC and Co, are used as the basis and other carbides such as TiC, TaC and so forth are added to WC, while other binders such as Mo, Ni, Fe and so forth are added to Co, a group of composites, called cermets (ceramics-metals), could be developed. For traditional hard metals, including cermets, the main preparing process is sintering, also allowing for a minute amount of the cemented phase to be incorporated.

However, the composite prepared from the above could be with a variety of choices, and not all the composite having a high hardness and a high toughness can be prepared by using all of the strengthening phase and the cemented phase materials. Therefore, if some certain strengthening materials and some certain cemented materials could possibly result in a composite with a high hardness and a high toughness such a solution undoubtedly might advance the development of the corresponding technology.

SUMMARY OF THE INVENTION

The disclosure is related to a composite having one or a plurality of principal strengthening compounds and at least one principal refractory metal, and specifically, to a suitable combination of binary to senary borides and/or carbides with one or more principal cemented refractory metal(s) with few other elements so as to prepare a composite with high hardness and high toughness.

The composition of the disclosed composite is two or three principal strengthening compounds and at least one principal cemented refractory metal. The principal strengthening compounds is selected from borides or carbides. The mole fraction of the principal strengthening compounds and the mole fraction of the principal cemented refractory metal are different.

Specifically, the principal cemented refractory metal is Nb, Ta, Mo and W.

Specifically, the boride is TiB₂ and ZrB₂.

Specifically, the carbide is TiC, VC, ZrC, HfC, WC, NbC and TaC.

The composition of the disclosed composite in another embodiment is two to six principal strengthening compounds and a principal cemented refractory metal. The principal strengthening compounds is selected from carbides, and the principal cemented refractory metal is selected from W.

Specifically, the carbide is TiC, ZrC, HfC, VC, NbC, TaC and WC.

Specifically, the mole fraction of the total principal strengthening compounds is 60 mol %, and the mole fraction of the principal cemented refractory metal is 40 mol %.

The composition of the disclosed composite in another embodiment is two to six principal strengthening compounds and one or two principal cemented refractory metal. The principal strengthening compounds is selected from carbides. The mole fraction of the principal strengthening compounds and the mole fraction of the principal cemented refractory metal are different.

Specifically, the principal cemented refractory metal is selected from Mo, W, Re and Ta.

Specifically, the carbide is selected from TiC, VC, ZrC, HfC, WC, NbC and TaC.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a flow chart of the process for preparing a composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to one embodiment of the disclosure.

FIG. 2A is a schematic diagram of the serial number and the composition of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the first embodiment of the disclosure;

FIG. 2B is a schematic diagram of the serial number and the composition of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the second embodiment of the disclosure;

FIG. 2C is a schematic diagram of the serial number and the composition of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the third embodiment of the disclosure;

FIG. 2D is a schematic diagram of the serial number and the composition of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the fourth embodiment of the disclosure;

FIG. 3A is a schematic diagram of the mechanical properties of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the first embodiment of the disclosure;

FIG. 3B is a schematic diagram of the mechanical properties of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the second embodiment of the disclosure;

FIG. 3C is a schematic diagram of the mechanical properties of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the third embodiment of the disclosure;

FIG. 3D is a schematic diagram of the mechanical properties of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the fourth embodiment of the disclosure;

FIG. 4A is a schematic diagram of the serial number and the composition of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the fifth embodiment of the disclosure;

FIG. 4B is a schematic diagram of the serial number and the composition of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the sixth embodiment of the disclosure;

FIG. 4C is a schematic diagram of the serial number and the composition of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the seventh embodiment of the disclosure;

FIG. 4D is a schematic diagram of the serial number and the composition of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the eighth embodiment of the disclosure;

FIG. 5A is a schematic diagram of the mechanical properties of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the fifth embodiment of the disclosure;

FIG. 5B is a schematic diagram of the mechanical properties of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the sixth embodiment of the disclosure;

FIG. 5C is a schematic diagram of the mechanical properties of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the seventh embodiment of the disclosure;

FIG. 5D is a schematic diagram of the mechanical properties of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the eighth embodiment of the disclosure;

FIG. 6A is a schematic diagram of the serial number and the composition of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the ninth embodiment of the disclosure;

FIG. 6B is a schematic diagram of the serial number and the composition of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the tenth embodiment of the disclosure;

FIG. 6C is a schematic diagram of the serial number and the composition of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the eleventh embodiment of the disclosure;

FIG. 6D is a schematic diagram of the serial number and the composition of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the twelfth embodiment of the disclosure;

FIG. 6E is a schematic diagram of the serial number and the composition of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the thirteenth embodiment of the disclosure;

FIG. 6F is a schematic diagram of the serial number and the composition of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the fourteenth embodiment of the disclosure;

FIG. 7A is a schematic diagram of the mechanical properties of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the ninth embodiment of the disclosure;

FIG. 7B is a schematic diagram of the mechanical properties of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the tenth embodiment of the disclosure;

FIG. 7C is a schematic diagram of the mechanical properties of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the eleventh embodiment of the disclosure;

FIG. 7D is a schematic diagram of the mechanical properties of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the twelfth embodiment of the disclosure;

FIG. 7E is a schematic diagram of the mechanical properties of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the thirteenth embodiment of the disclosure; and

FIG. 7F is a schematic diagram of the mechanical properties of the composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to the fourteenth embodiment of the disclosure.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

The following description with reference to the accompanying drawings is provided to clearly and completely explain the exemplary embodiments of the disclosure.

According to the disclosure, the feature is to select appropriate binary to senary principal strengthening compounds (borides and/or carbides) and unitary to binary principal cemented refractory metal so as to prepare a composite having a high hardness and a high toughness. According to the disclosure, there are three modes of combinations of the principal strengthening compounds and the principal cemented refractory metal, all of which can prepare a composite having a high hardness and a high toughness through sintering or smelting process.

Although the product prepared by the sintering remains higher in hardness and strength under low temperatures, the process is too complicated and the toughness of the prepared product is not as desired. Thus, although it is feasible to prepare the principal strengthening compounds and the principal refractory metals by sintering, it is simpler and more rapid than sintering if they are prepared by the smelting. In addition, the metallurgical microstructure of the product prepared by the smelting is a typical dendritic structure, which has 100% relative density and is good in toughness. Therefore, the disclosure is explained by the embodiments employing the smelting. However, a composite with a high hardness and a high toughness can still be prepared by the sintering if necessary according to the disclosure.

As shown in FIG. 1, when using the smelting, the method may include the following:

(1) Vacuum arc smelting furnace is used for preparing composite, the principal strengthening compound powders and bulk metal are weighted and placed evenly in a water-cooled copper mold (101);

(2) The furnace cover is covered and the pressure is reduced to 2.4×10⁻² torr, pure argon is incorporated until the pressure is about 8.0 torr, and the pressure is reduced again, the purging process is repeated for three times, and then the smelting process is performed (102); and

(3) The smelting current is 550 ampere, after the smelting and the composite is cooled completely, the composite block is turned upside down and is smelted again; such flipping and smelting may be repeated for 4 times for ensuring all the elements in the specimen are uniformly mixed; when the composite is cooled completely again, the vacuum may be exhausted and the ingot is obtained as a molded specimen (103).

According to the first embodiment of the disclosure, the composite is with two or three principal strengthening compounds and a principal cemented refractory metal, and the principal strengthening compounds is selected from borides or carbides. The mole fraction of the principal strengthening compounds and the mole fraction of the principal cemented refractory metal are different, the principal cemented refractory metal is selected from Nb, Ta, Mo and W, the boride is selected from TiB₂ and ZrB₂ and the carbide is selected from TiC, VC, ZrC, HfC, WC, NbC and TaC.

According to FIG. 2A, the used boride is TiB₂ (B1) and ZrB₂ (B2) and the used principal cemented refractory metal is Nb, Ta, Mo and W. According to the figure, it is the composite combined by a unitary boride as the principal strengthening compound and a unitary principal cemented refractory metal. Further, FIG. 3A shows the hardness (HV) and the toughness (K_(IC)) of the composite composed of the unitary boride and the unitary principal cemented refractory metal.

According to FIG. 2B, the used boride is TiB₂ (B1) and ZrB₂ (B2) and the used carbide is TiC (C1), VC (C2), ZrC (C3), HfC (C4), WC (C5), NbC (C6) and TaC (C7). The difference between W and W′ is the mole fraction. According to the figure, it is the composite combined by unitary boride as the principal strengthening compound and unitary or binary carbide as the principal strengthening compound. Further, FIG. 3B shows the hardness (HV) and the toughness (K_(IC)) of the composite having the unitary boride or the unitary or binary carbide as the principal strengthening compound and the unitary principal cemented refractory metal as the principal cemented refractory metal.

According to FIG. 2C, the boride is TiB₂ (B1) and the carbide is TiC (C1), VC (C2), ZrC (C3), HfC (C4), WC (C5), NbC (C6) and TaC (C7). According to the figure, it is the composite combined by a unitary boride (the principal strengthening compound), a unitary carbide (the principal strengthening compound) and a unitary principal cemented refractory metal (the principal cemented refractory metal). Further, FIG. 3C shows the hardness (HV) and the toughness (K_(IC)) of the composite having the unitary boride (the principal strengthening compound), the unitary carbide (the principal strengthening compound) and the unitary principal cemented refractory metal (the principal cemented refractory metal).

According to FIG. 2D, the used boride is ZrB₂ (B2) and the used carbide is TiC (C1), VC (C2), ZrC (C3), HfC (C4), WC (C5), NbC (C6) and TaC (C7). According to the figure, it is the composite combined by a unitary boride (the principal strengthening compound), a unitary carbide (the principal strengthening compound) and a unitary principal cemented refractory metal (the principal cemented refractory metal). Further, FIG. 3D shows the corresponding hardness (HV) and the toughness (K_(IC)) of the composite having the unitary boride (the principal strengthening compound), the unitary carbide (the principal strengthening compound) and the unitary principal cemented refractory metal (the principal cemented refractory metal).

According to FIGS. 3A to 3D, when diborides (TiB₂ and ZrB₂) are incorporated into the system, the mechanical properties of most of the specimens may improve. Moreover, in C1B2 to C7B2, all of the hardness of the specimens significantly improves.

According to the second embodiment of the disclosure, the composite is composed of two to six principal strengthening compounds and the principal cemented refractory metal. The principal strengthening compounds may be selected from carbides, the principal cemented refractory metal may be selected from W. The mole fraction of the total principal strengthening compounds is 60 mol %, and the mole fraction of the principal cemented refractory metal is 40 mol %. In addition, the carbide is TiC, ZrC, HfC, VC, NbC, TaC and WC.

According to FIG. 4A, the used carbide is TiC (T1˜T9 is defined by the mole fraction) (the chemical formula is (TiC)_(0.x)W_((1-0.x)), x=1˜9) and the used principal cemented refractory metal is W. According to the figure, it is the composite combined by a unitary carbide (the principal strengthening compound) and a unitary W (the principal cemented refractory metal). Further, FIG. 5A shows the hardness (HV) and the toughness (K_(IC)) of the composite composed of the unitary carbide (the principal strengthening compound) and the unitary W (the principal cemented refractory metal). According to the figure, W has better performance in both hardness and toughness when the mole fraction of W is 40 mol %. Therefore, the following embodiments are with 40 mole % of W for the illustration purpose.

According to FIG. 4B, the carbide is TiC (C1), VC (C2), ZrC (C3), HfC (C4), WC (C5), NbC (C6) and TaC (C7), and S indicates W with 40 mole %. According to the figure, it is the composite combined by a unitary carbide (the principal strengthening compound) and a unitary W (the principal cemented refractory metal). Further, FIG. 5B shows the hardness (HV) and the toughness (K_(IC)) of the composite composed of the unitary carbide (the principal strengthening compound) and the unitary W (the principal cemented refractory metal).

According to FIG. 4C, NT1 indicates that the used carbide is NbC and TaC, NT2 indicates that the used carbide is NbC, TaC and TiC. NT2a, NT2b, NT2c and NT2d may have different mole ratios of the used carbide compared to NT2. In the meantime, NT2e indicates that the used carbide is TiC, ZrC, HfC, NbC and TaC, NT3 indicates that the used carbide is NbC, TaC, TiC and WC. Similarly, NT3a and NT3b may have different mole ratios of the used carbide compared with NT3. Also, NT4 indicates that the used carbide is NbC, TaC, TiC, WC and VC, and NT5 indicates that the used carbide is NbC, TaC and WC. According to the figure, it is the composite combined by a binary or more of carbide (the principal strengthening compound) and a unitary W (the principal cemented refractory metal). Further, FIG. 5C shows the hardness (HV) and the toughness (K_(IC)) of the composite composed of the binary or more of carbide (the principal strengthening compound) and the unitary W (the principal cemented refractory metal).

According to FIG. 4D, WC 1 indicates that the used carbide is TiC and WC, WC2 indicates that the used carbide is TiC, ZrC, HfC and WC, HE1 indicates that the used carbide is TiC, ZrC, HfC, NbC, TaC and WC, HE2 indicates that the used carbide is TiC, ZrC, HfC, VC, NbC, TaC and WC, HE3 has different mole ratio of the used carbide, as compared with HE2, MW1 indicates that the used carbide is TiC, NbC and TaC, MW2 indicates that the used carbide is TiC, NbC, TaC, WC, MW3 and MW4 have different mole ratio of the used carbide, as compared with MW2, MW5 indicates that the used carbide is NbC, and MW 6 indicates that the used carbide is TaC. According to the figure, it is the composite combined by a unitary or more of carbide (the principal strengthening compound) and a unitary W (the principal cemented refractory metal). Further, FIG. 5D shows the hardness (HV) and the toughness (K_(IC)) of the composite composed of the unitary or more of carbide (the principal strengthening compound) and the unitary W (the principal cemented refractory metal).

According to FIGS. 5A to 5D, NT3a and NT3b have the best performance in both hardness and toughness. The two specimens have great performance in rear and cutting resistance. In addition, most of the composite in the disclosure may be with hardness greater than 1000 HV. Thus, the disclosure is significantly better than most of the commercial ultra hard alloy.

According to the third embodiment of the disclosure, the composite is with two to six principal strengthening compounds and one or two of the principal cemented refractory metals, and the principal strengthening compounds may be selected from carbides. And the mole fraction of the principal strengthening compounds and the mole fraction of the principal cemented refractory metal are different, the principal cemented refractory metal is selected from Mo, W, Re and Ta, and the carbide is TiC, VC, ZrC, HfC, WC, NbC and TaC.

According to FIG. 6A, the used carbide is TiC (A) and the used principal refractory metal is Mo (M). According to the figure, it is the composite combined by a unitary carbide (the principal strengthening compound) and a unitary principal cemented refractory metal (the principal cemented refractory metal). Further, FIG. 7A shows the hardness (HV) and the toughness (K_(IC)) of the composite composed of the unitary carbide (the principal strengthening compound) and the unitary principal cemented refractory metal (the principal cemented refractory metal).

According to FIG. 6B, the used carbide is TiC (A), VC (B), ZrC (C), HfC (D), WC (E), NbC (F) and TaC (G), and the used principal refractory metal is Mo (M). According to the figure, it is the composite combined by different unitary carbides (the principal strengthening compound) and a unitary principal cemented refractory metal (the principal cemented refractory metal). Further, FIG. 7B shows the hardness (HV) and the toughness (K_(IC)) of the composite with different unitary carbides (the principal strengthening compound) and the unitary principal cemented refractory metal (the principal cemented refractory metal).

According to FIG. 6C, the used carbide is TiC (A), VC (B), ZrC (C), HfC (D), WC (E), NbC (F) and TaC (G), and the used principal refractory metal is Mo (Mo) and W (W). According to the figure, it is the composite combined by different binary or more of carbides (the principal strengthening compound) and a unitary or binary principal cemented refractory metal (the principal cemented refractory metal). Further, FIG. 7C shows the hardness (HV) and the toughness (K_(IC)) of the composite composed of different binary or more of carbides (the principal strengthening compound) and the unitary or binary principal cemented refractory metal (the principal cemented refractory metal).

According to FIG. 6D, the used carbide is NbC (F) and TaC (G), and the used principal refractory metal is W (W) and Re (R). According to the figure, it is the composite combined by a binary carbide (the principal strengthening compound) and a unitary or binary principal cemented refractory metal (the principal cemented refractory metal). Further, FIG. 7D shows the hardness (HV) and the toughness (K_(IC)) of the composite composed of the binary carbide (the principal strengthening compound) and the unitary or binary principal cemented refractory metal (the principal cemented refractory metal).

According to FIG. 6E, the used carbide is NbC (F) and TaC (G), and the used principal refractory metal is W (W) and Ta (T). According to the figure, it is the composite combined by a binary carbide (the principal strengthening compound) and a unitary or binary principal cemented refractory metal (the principal cemented refractory metal). Further, FIG. 7E shows the hardness (HV) and the toughness (K_(IC)) of the composite composed of the binary carbide (the principal strengthening compound) and the unitary or binary principal cemented refractory metal (the principal cemented refractory metal).

According to FIG. 6F, the used carbide is NbC (F), TaC (G) and TiC (A), and the used principal refractory metal is W (W) and Mo (M). According to the figure, it is the composite combined by a ternary carbide (the principal strengthening compound) and a unitary or binary principal cemented refractory metal (the principal cemented refractory metal). Further, FIG. 7F shows the hardness (HV) and the toughness (K_(IC)) of the composite composed of the ternary carbide (the principal strengthening compound) and the unitary or binary principal cemented refractory metal (the principal cemented refractory metal).

As shown in FIGS. 7A to 7F, it is found out when W is the main part of the cemented phase and a small amount of Mo is added, the performance may be more desired when the hardness and the toughness increase, as compared to pure W. This phenomena is generated from the layered structure when the W content increases; in addition, in a binary carbide system, the incorporation of Re can improve the strength of the specimen at a high temperature, and W could be a better alternative other than Re. Among the third composites of the disclosure, the ratio of the composite, which may dictate the hardness, is low, such that they are greater than their counterparts such as WC—Co.

According to the disclosure, as compared to traditional technologies, the composite composed of one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal of the disclosure has the following advantages:

1. The disclosure can select appropriate binary to senary principal strengthening compounds and unitary to binary (few elements) of the principal cemented refractory metal so as to prepare a composite having a high hardness and a high toughness.

2. As compared to traditional cermet composites, the composite of the disclosure has a high hardness and a high toughness, and it is not prepared with equal mole during the process

Note that the specifications relating to the above embodiments should be construed as exemplary rather than as limitative of the present disclosure. The equivalent variations and modifications on the structures or the process by reference to the specification and the drawings of the disclosure, or application to the other relevant technology fields directly or indirectly should be construed similarly as falling within the protection scope of the disclosure. 

What is claimed is:
 1. A composite having one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal, wherein the composition of the composite is two or three principal strengthening compounds and a principal cemented refractory metal, and the principal strengthening compounds is selected from borides or carbides, wherein the mole fraction of the principal strengthening phase compounds and the mole fraction of the principal cemented refractory metal are different.
 2. The composite composed of one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to claim 1, wherein the principal cemented refractory metal is selected from Nb, Ta, Mo and W.
 3. The composite composed of one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to claim 1, wherein the boride is selected from TiB₂ and ZrB₂.
 4. The composite composed of one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to claim 1, wherein the carbide is selected from TiC, VC, ZrC, HfC, WC, NbC and TaC.
 5. A composite composed of one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal, wherein the composition of the composite is two to six principal strengthening compounds and a principal cemented refractory metal, the principal strengthening compounds is selected from carbides, and the principal cemented refractory metal is selected from W.
 6. The composite composed of one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to claim 5, wherein the carbide is selected from TiC, ZrC, HfC, VC, NbC, TaC and WC.
 7. The composite composed of one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal according to claim 5, wherein the mole fraction of the total principal strengthening compounds is 60 mol %, and the mole fraction of the principal cemented refractory metal is 40 mol %.
 8. A composite composed of one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal, wherein the composition of the composite is two to six principal strengthening compounds and one or two principal cemented refractory metal(s), the principal strengthening compounds is selected from carbides, wherein the mole fraction of the principal strengthening compounds and the mole fraction of the principal cemented refractory metal are different.
 9. The composite composed of one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal(s) according to claim 8, wherein the principal cemented refractory metal is selected from Mo, W, Re and Ta.
 10. The composite composed of one or a plurality of principal strengthening compounds and at least one principal cemented refractory metal(s) according to claim 8, wherein the carbide is selected from TiC, VC, ZrC, HfC, WC, NbC and TaC. 